Concentrated Photovoltaic System Modules Using III-V Semiconductor Solar Cells

ABSTRACT

A solar cell module to convert light to electricity. The module may include a housing with a first side and an opposing spaced-apart second side. A plurality of lenses may be positioned on the first side of the housing, and a plurality of solar cell receivers may be positioned on the second side of the housing. Each of the plurality of solar cell receivers may include a III-V compound semiconductor multifunction solar cell. Each may also include a bypass diode coupled with the solar cell. At least one optical element may be positioned above the solar cell to guide the light from one of the lenses onto the solar cell. Each of said solar cell receivers may be disposed in an optical path of one of the lenses. The lens and the at least one optical element may concentrate the light onto the respective solar cell by a factor of 1000 or more to generate in excess of 25 watts of peak power.

RELATED APPLICATIONS

The present application is a continuation-in-part of U.S. patent application Ser. No. 12/069,642 filed Feb. 11, 2008 and herein incorporated by reference in its entirety. The disclosure of this application is related to co-pending U.S. patent application Ser. No. 12/485,684, herein incorporated by reference in its entirety.

BACKGROUND

Satisfying the world's growing demand for energy is one of the most significant challenges facing society. At present, about 85% of the energy produced in the United States comes from fossil fuels. Given that the supply of such fuels is on the decline, their prices continue to rise, and the resultant greenhouse gases may contribute to global warming, there is a need to develop new technologies that are economically feasible and environmentally friendly.

Solar energy is one technology for power generation that is clean, quiet and renewable. It is also plentiful: with an average of roughly 125,000 terawatts of solar energy reaching the planet at any given time, solar technology can potentially generate a significant amount of energy.

Solar cells are used to convert solar or radiant energy into electricity. Historically, solar power (both in space and terrestrially) has been predominantly provided by silicon solar cells. In the past several years, however, high-volume manufacturing of high-efficiency III-V multijunction solar cells has enabled the consideration of this alternative technology for terrestrial power generation. Compared to Si, III-V multijunction cells are generally more radiation resistant and have greater energy conversion efficiencies, but they tend to cost more. Some current III-V multijunction cells have energy efficiencies that exceed 27%, whereas silicon technologies generally reach only about 17% efficiency. Under concentration, some current III-V multijunction cells have energy efficiencies that exceed 37%. When the need for very high power or smaller solar arrays are paramount in a spacecraft or other solar energy system, multijunction cells are often used instead of, or in hybrid combinations with, Si-based cells to reduce the array size.

Generally speaking, the multijunction cells are of n-on-p polarity and are composed of InGaP/(In)GaAs/Ge compounds. III-V compound semiconductor multijunction solar cell layers can be grown via metal-organic chemical vapor deposition (MOCVD) on Ge substrates. The use of the Ge substrate permits a junction to be formed between n- and p-Ge. The solar cell structures can be grown on 100-mm diameter (4 inch) Ge substrates with an average mass density of about 86 mg/cm.sup.2. In some processes, the epitaxial layer uniformity across a platter that holds 12 or 13 Ge substrates during the MOCVD growth process is better than 99.5%. Each wafer typically yields two large-area solar cells. The cell areas that are processed for production typically range from 26.6 to 32.4 cm². The epi-wafers can be processed into complete devices through automated robotic photolithography, metallization, chemical cleaning and etching, antireflection (AR) coating, dicing, and testing processes. The n- & p-contact metallization is typically comprised of predominately Ag with a thin Au cap layer to protect the Ag from oxidation. The AR coating is a dual-layer TiO_(x)/Al₂O₃ dielectric stack, whose spectral reflectivity characteristics are designed to minimize reflection at the coverglass-interconnect-cell (CIC) or solar cell assembly (SCA) level, as well as, maximizing the end-of-life (EOL) performance of the cells.

In some multifunction cells, the middle cell is an InGaAs cell as opposed to a GaAs cell. The indium concentration may be in the range of about 1.5% for the InGaAs middle cell. In some implementations, such an arrangement exhibits increased efficiency. The InGaAs layers are substantially perfectly lattice-matched to the Ge substrate.

Regardless of the type of cell used, a known problem with solar energy systems is that individual solar cells can become damaged or shadowed by an obstruction. For example, damage can occur as a result of exposure of a solar cell to harsh environmental conditions. The current-carrying capacity of a panel having one or more damaged or shadowed solar cells is reduced, and the output from other panels in series with that panel reverse biases the damaged or shadowed cells. The voltage across the damaged or shadowed cells thus increases in a reverse polarity until the full output voltage of all of the panels in the series is applied to the damaged or shadowed cells in the panel concerned. This causes the damaged or shadowed cells to breakdown.

As a solar cell system for terrestrial applications has thousands of solar cells, its voltage output is normally in the range of hundreds of volts, and its current output is in the range of tens of amperes. At these output power levels, if the solar cell terminals are not protected, uncontrollable electric discharge in the form of sparks tends to occur, and this can cause damage to the solar cells and to the entire system.

SUMMARY

The present application is directed to a solar cell module to convert light to electricity. The module may include a housing with a first side and an opposing spaced-apart second side. A plurality of lenses may be positioned on the first side of the housing, and a plurality of solar cell receivers may be positioned on the second side of the housing. Each of the plurality of solar cell receivers may include a III-V compound semiconductor multijunction solar cell. Each may also include a bypass diode coupled with the solar cell. At least one optical element may be positioned above the solar cell to guide the light from one of the lenses onto the solar cell. Each of said solar cell receivers may be disposed in an optical path of one of the lenses. The lens and the at least one optical element may concentrate the light onto the respective solar cell by a factor of 1000 or more to generate in excess of 25 watts of peak power.

The various aspects of the various embodiments may be used alone or in any combination, as is desired.

BRIEF DESCRIPTION OF THE DRAWINGS

The present invention will be now described more fully hereinafter with reference to the accompanying drawings, in which some, but not all embodiments of the invention are shown. Drawings illustrating the embodiments are not-to-scale schematic representations. For the purpose of the present description and of the appended claims, all ranges include the maximum and minimum points disclosed and include any intermediate ranges therein, which may or may not be specifically enumerated herein.

FIG. 1 is a perspective view of an implementation of a solar cell module.

FIG. 2 is a perspective view of an implementation of a secondary optical element.

FIG. 3 is a partially exploded perspective view of an implementation of a solar cell receiver.

FIG. 4 is a partially exploded perspective view illustrating the solar cell and the metalized ceramic substrate of FIG. 3 in more detail.

FIG. 5 is a sectional view of the solar cell, the metalized ceramic substrate and the heat sink along line X-X′ of FIG. 3.

DETAILED DESCRIPTION

FIG. 1 illustrates an implementation of a solar cell module 200 comprising an array of lenses 210 and corresponding solar cell receivers 300. Each one of the lenses 210 is aligned with one of the solar cell receivers 300. The solar cell module 200 may include various numbers of lenses 210 and solar cell receivers 300. FIG. 1 include a module 200 with fifteen lenses 210 and solar cell receivers 300 aligned in a 3×5 array.

The lenses 210 are formed on a continuous sheet 211 of optical material (e.g., acrylic). In some implementations, regions of the sheet 211 not formed into the lenses 210 are made partially or entirely opaque. By forming the lenses 210 out of a continuous sheet 211, costs can be decreased substantially. First, by producing the lenses 210 on large sheets, production costs are decreased. Second, assembly costs are decreased because only one item (i.e., the sheet 211 of lenses) needs to be aligned with the solar cell receivers 300. In this implementation, the sheet 211 lies atop an alignment frame 221 of a housing 220.

One or more vent openings 228 may be positioned in the housing 220. The openings 228 may be positioned to facilitate air flow through the housing 220. In one embodiment, the openings 228 are positioned in the sidewalls of the housing 220 and about 3″ below the lenses 210. The size of the openings 228 may vary. In one embodiment, each opening has a circular shape with a diameter of about 1″. A cover 229 may extend across the openings 228 and act as a filter to impede the introduction of moisture and debris into the housing 220. The cover 229 may be constructed of a variety of materials, including but not limited to GORETEX, nylon, and polyvinylidene.

The frame 221 may include a plurality of frame alignment elements, such as holes. The alignment elements may be threaded or otherwise adapted to receive a fastener. The sheet 211 may include sheet alignment elements such as pins, screws or other hardware that align and couple with the frame alignment elements. The frame alignment elements and the sheet alignment elements are located such that by coupling the sheet alignment elements with the frame alignment elements, each of the lenses 210 is aligned with a corresponding solar cell receiver 300. The alignment elements are located generally in a center point defined by four of the lenses 210. In one embodiment, an alignment element is located in a center point defined by lenses 210 a, 210 b, 210 c, and 210 d. Another alignment element may be located in a center point defined by four other lenses 210. This pattern of locating the alignment elements in a center point defined by four lenses can continue along the entire sheet 211.

In some implementations, the surface 222 of the housing 220 comprises alignment features that ensure that each of the solar cell receivers 300 is located in a predetermined position. These features may couple with each of the solar cell receivers 300.

In some implementations, each of the lenses 210 is a Fresnel lens. The corresponding solar cell receiver 300 is positioned on the surface 222 at an opposite end of the housing 220. Each of the solar cell receivers 300 includes a corresponding solar cell 310 disposed in the optical path of the corresponding lens 210, i.e., such that the corresponding solar cell 310 receives light that passes through the corresponding lens 210. In some implementations, additional optical elements are employed to place the solar cell in the optical path of the lens. For example, secondary optical elements 400 correspond with each pair of the solar cell receivers 300 and the lenses 210. The secondary optical elements 400 gather the light from the lens 210 and direct it into the solar cell 310 of the solar cell receiver 300. In some implementations, each of the solar cell receivers 300 is provided with a corresponding secondary optical element 400.

Another optical element includes a concentrator 450 that is positioned between each of the pairs of solar cell receivers 300 and lenses 210. The concentrator concentrates the light onto the solar cell 310.

While some Fresnel lenses can concentrate more sunlight than some convex lenses, implementations may use any type of lens 210 that concentrates the incident sunlight. For example, any of lenses 210 may take the form of a biconvex lens, a plano-convex lens, or a convex-concave lens. The lenses 210 may also comprise a multi-layer anti-reflective coating. In a module 200, each of the lenses 210 may be the same, or the module 200 may include two or more different lenses 210.

A distance X measured between the sheet 211 comprising the lenses 210 and the solar cells 310 of the corresponding solar cell receivers 300 may be chosen based on the focal length of the lenses 210. In some implementations the housing 220 is arranged so that the solar cell 310 each respective solar cell receiver 300 is disposed at or about the focal point of the respective lens 210. In some implementations, the focal length of each of the lenses 210 is between about 25.4cm (10 inches) and 76.2 cm (30 inches). In some implementations, the focal length of each lens 210 is between about 38.1 cm (15 inches) and 50.8 cm (20 inches). In some implementations, the focal length of each lens 210 is about 40.085 cm (17.75 inches). In some implementations, the focal length of each lens 210 varies, and the housing 220 provides multiple different distances (e.g., those that are greater and/or lesser than the distance X) between the sheet 211 and the surface 222.

The housing 220 and the lens sheet 211 may form an enclosed interior space that protects the solar cell receivers 300 from the environment.

Some implementations of the lenses 210 concentrate incident sunlight to 1000 times normal concentration (i.e., 1000 Suns) or more. Other implementations may include other concentrations. Generally speaking, conversion efficiency of solar energy into electricity increases under concentrated illumination. For example, at about 1000 Suns, a single solar cell receiver can generate 25 watts or more of electrical power. In another example, at about 470 Suns or more, a single solar cell module can generate 14 watts or more of electrical power. The amount of electrical power a module can produce can vary depending on, for example, the combination of solar cell characteristics (e.g., size, composition) and properties of the associated optics (e.g., concentration, focus, alignment).

In some implementations, the solar cells 310 of each of the respective solar cell receivers 300 is a triple-junction III-V solar cell, with each of the three sub-cells arranged in series. In applications where multiple solar cell modules 200 are employed, the receivers 210 of the solar cell modules 200 are typically electrically connected together in series. However, other applications may utilize parallel or series-parallel connection. For example, receivers 300 within a given module 200 can be electrically connected together in series, but the modules 200 are connected to each other in parallel.

As previously explained, a secondary optical element (“SOE”) 400 may be positioned between the lens 210 and the corresponding solar cell 310. An implementation of an SOE is illustrated in FIG. 2. The SOE 400 is disposed inside the housing 220 of the solar cell module 200 and is generally designed to collect solar energy concentrated by one of the corresponding lenses 210. In some implementations, each of the solar cell receivers 300 has a respective SOE 400. Other modules 200 may include less than each solar cell receiver 300 including an SOE 400.

The SOE 400 comprises an optical element 401 with an optical inlet 402 and an optical outlet 403, a body 404 and mounting tabs 405. The SOE 400 is mounted such that the optical element 401 is disposed above the solar cell 310 of the corresponding solar cell receiver 300. While it may vary depending on the implementation, the SOE 400 is mounted such that the optical outlet 403 is about 0.5 millimeters from the solar cell 310 (e.g., dimension 406 is about 0.5 millimeters). In some implementations, mounting tabs 405 couple to the face 222 of the housing 220. The SOE 400 may be made of metal, plastic, or glass or other materials.

In some implementations, the optical element 401 has a generally square cross section that tapers from the inlet 402 to the outlet 403. The inside surface 407 of the optical element reflects light downward toward the outlet 403. The inside surface 407 is, in some implementations, coated with silver or another material for high reflectivity. In some cases, the reflective coating is protected by a passivation coating such as SiO₂ to protect against oxidation, tarnish or corrosion. The path from the optical inlet 402 to the optical outlet 403 forms a tapered optical channel that catches solar energy from the corresponding lens 210 and guides it to the corresponding solar cell 310. As shown in this implementation, the SOE 400 comprises an optical element 401 having four reflective walls. In other implementations, different shapes (e.g., three-sided to form a triangular cross-section) may be employed.

Under ideal conditions, the corresponding lens 210 associated with the SOE 400 focuses the light directly to the solar cell 310 without the light hitting against the SOE 400. In most circumstances, the lens 210 does not focus light directly on the solar cell 310. This may occur due to a variety of causes, including but not limited to chromatic aberration of a refractive lens design, misalignment of the solar cell 310 relative to the lens 210 during construction, misalignment during operation due to tracker error, structural flexing, and wind load. Thus, under most conditions, the lens 210 focuses the light such that it reflects off the SOE 400. The difference between an ideal setup and a misaligned setup may be a minor variation in the positioning of the lens 210 of less than 1°. The SOE 400 therefore acts as a light spill catcher to cause more of the light to reach the solar cell 310 in circumstances when the corresponding lens 210 does not focus light directly on the solar cell 310. The SOE 400 can include a reflective multi-layer intermediate region such as the kind disclosed in U.S. patent application Ser. No. 12/402,814 filed on Mar. 12, 2009, which is incorporated herein by reference in its entirety.

The reflective multi-layer intermediate region can be formed from different materials and have different optical characteristics so that the reflectivity of the light beams off the SOE 400 and transmitted to the solar cell 310 optimizes the aggregate irradiance on the surface of the solar cell 310 over the incident solar spectrum. For example, in some implementations, the inner surface of the 407 can be coated with silver or another material for high reflectivity. In some cases, the reflective coating is protected by a passivation coating such as SiO₂ to protect the SOE 400 against oxidation, tarnish or corrosion. The SOE 400 may also homogenize (e.g., mix) the light. In some cases, it also has some concentration effect.

In some implementations, the optical inlet 402 is square-shaped and is about 49.60 mm×49.60 mm (dimension 408), the optical outlet is square-shaped and is about 9.9 mm×9.9 mm (dimension 409) and the height of the optical element is about 70.104 mm (dimension 410). The dimensions 408, 409, and 410 may vary with the design of the solar cell module 200 and the solar cell receiver 300. For example, in some implementations the dimensions of the optical outlet 403 are approximately the same as the dimensions of the solar cell 310. For an SOE 400 having these dimensions, the half inclination angle is 15.8 degrees.

Each of the solar cells 310 may be a triple-junction III-V compound semiconductor solar cell which comprises a top cell, a middle cell and a bottom cell arranged in series. In another embodiment, the solar cells 310 are multijunction solar cells having n-on-p polarity and is composed of InGaP/(In)GaAs III-V compounds on a Ge substrate. In each case, the solar cells 310 are positioned to receive focused solar energy from SOE 400 and/or the corresponding lens 210.

An anti-reflective coating may be disposed on the solar cell 310. The anti-reflective coating may be a multi-layer antireflective coating providing low reflectance over a certain wavelength range, e.g., 0.3 to 1.8 μm. An example of an anti-reflective coating is a dual-layer TiO_(x)/Al₂O₃ dielectric stack.

As illustrated in FIG. 3, the tabs 405 of the SOE 400 may be configured for attaching the SOE 400 to a bracket 230 via one or more fasteners 231. The bracket 230 is provided for mounting the SOE 400 to a heat sink 350 via one or more fasteners 232. The bracket 230 is thermally conductive so that heat energy generated by the SOE 400 during operation can be transferred to the heat sink 350 and dissipated.

In one embodiment as shown in FIGS. 3 and 4, a concentrator 450 is disposed between the outlet 403 of the SOE 400 and the solar cell 310. The concentrator 450 is preferably glass and has an optical inlet 451 and an optical outlet 452. In one embodiment, the concentrator 450 is solid glass. The concentrator 450 amplifies the light exiting the SOE 400 and directs the amplified light toward the solar cell 310. In some implementations, the concentrator 450 has a generally square cross section that tapers from the inlet 451 to the outlet 452. In some implementations, the optical inlet 451 of the concentrator 450 is square-shaped and is about 2 cm×2 cm and the optical outlet 452 is about 0.9 cm×0.9 cm. The dimensions of the concentrator 450 may vary with the design of the solar cell module 200 and the solar cell receiver 300. For example, in some implementations the dimensions of the optical outlet 452 are approximately the same as the dimensions of the solar cell 310. In one embodiment, the concentrator 450 is a 2× concentrator. The bottom surface of the concentrator 450 can be directly attached to the upper surface of the solar cell 310 using an adhesive such as a silicone adhesive. The solar cell 310 converts the incoming sunlight directly into electricity by the photovoltaic effect.

In some embodiments as illustrated in FIGS. 1 and 3, both an SOE 400 and a concentrator 450 are positioned along the optical path between the corresponding lens 210 and solar cell 310. Other embodiments may include just one of these optical elements positioned the optical path. Other embodiments may include neither of these elements along the optical path. Within a module 200, each of the lens 210/solar cell 310 pairs may include the same or different combination of elements for directing the light.

As illustrated in FIGS. 3 and 4, a bypass diode 360 is connected in parallel with the solar cell 310. In some implementations, the diode 360 is a semiconductor device such as a Schottky bypass diode or an epitaxially grown p-n junction. For purposes of illustration, the bypass diode 360 is a Schottky bypass diode. External connection terminals 361 and 362 are provided for connecting the solar cell 310 and the diode 360 to other devices, e.g., adjacent solar cell receivers (not illustrated).

The functionality of the bypass diode 360 can be appreciated by considering multiple solar cells 310 connected in series. Each solar cell 310 can be envisioned as a battery, with the cathode of each of the diodes 360 being connected to the positive terminal of the associated “battery” and the anode of each of the diodes 360 being connected to the negative terminal of the associated “battery.” When one of the serially-connected solar cell receivers 300 becomes damaged or shadowed, its voltage output is reduced or eliminated (e.g., to below a threshold voltage associated with the diode 360). Therefore, the associated diode 360 becomes forward-biased, and a bypass current flows only through that diode 360 (and not the solar cell 310). In this manner, the non-damaged or non-shadowed solar cell receivers 300 continue to generate electricity from the solar energy received by those solar cells. If not for the bypass diode 360, substantially all of the electricity produced by the other solar cell receivers would pass through the shadowed or damaged solar cell receiver, destroying it, and creating an open circuit within, e.g., the panel or array.

The solar cell receiver 300 also includes a ceramic substrate 370 such as an alumina substrate for mounting of the solar cell 310 and the heat sink 350 for dissipating heat generated by the solar cell 310 during operation.

FIG. 4 illustrates the solar cell 310 and the ceramic substrate 370 in more detail. The ceramic substrate 370 has metallized upper and lower surfaces 371 and 372. Both surfaces 371 and 372 of the ceramic substrate 370 are metallized to increase the heat transfer capacity of the ceramic substrate 370, enabling the solar cell receiver 300 to more adequately handle rapid temperature changes that occur due to abrupt changes in solar cell operating conditions. For example, the solar cell 310 generates heat energy when converting light to electricity. Having both the upper and lower surfaces 371 and 372 of the ceramic substrate 370 metallized provides for a faster transfer of the heat energy from the solar cell 310 to the heat sink 350 for dissipation. The opposite condition occurs when the solar cell 310 becomes suddenly shaded. That is, the solar cell 310 stops producing electricity and rapidly cools as does the SOE 400. The metallized upper and lower surfaces 371 and 372 of the ceramic substrate 370 prevent the solar cell 310 from cooling too rapidly by transferring heat energy from the heat sink 350 to the solar cell 310, and depending on the thermal conditions, to the SOE 400 as well. The increased heat transfer capacity of the solar cell receiver 300 reduces the amount of stress imparted to the interface between the solar cell 310 and the ceramic substrate 370 during rapid temperature changes, ensuring a reliable solar cell-to-substrate interface.

The metallized upper surface 371 of the ceramic substrate 370 is in contact with the solar cell 310 and has separated conductive regions 375 and 376 for providing isolated electrically conductive paths to the solar cell 310. The first conductive region 375 provides an anode electrical contact point for the solar cell 310 and the second conductive region 376 provides a cathode electrical contact point for the solar cell 310. The solar cell 310 has a conductive lower surface 372 out-of-view in FIG. 4, but visible in the cross-section of FIG. 5 that is positioned on and connected to the first conductive region 375 of the metallized upper surface 371 of the ceramic substrate 370. The opposing upper surface 311 of the solar cell 310 has a conductive contact area 312 connected to the second conductive region 376 of the ceramic substrate 370.

In one embodiment, the conductive lower surface 313 of the solar cell 310 forms an anode terminal of the solar cell 310 and the conductive contact area 312 disposed at the upper surface 311 of the solar cell 310 forms a cathode terminal. According to this embodiment, the conductive lower surface 313 of the solar cell 310 is positioned on the first conductive region 375 of the ceramic substrate 370 and electrically isolated from the second conductive region 376 to ensure proper operation of the solar cell 310. In one embodiment, the first conductive region 375 of the ceramic substrate 370 is at least partly surrounded on three sides by the second conductive region 376 about a periphery region of the ceramic substrate 370.

In one embodiment, the conductive contact area 312 disposed at the upper surface 311 of the solar cell 310 occupies the perimeter of the solar cell 310. In some implementations, the upper conductive contact area 312 can be smaller or larger to accommodate the desired connection type. For example, the upper conductive contact area 312 may touch only one, two or three sides (or portions thereof) of the solar cell 310. In some implementations, the upper conductive contact area 312 is made as small as possible to maximize the area that converts solar energy into electricity, while still allowing electrical connection. While the particular dimensions of the solar cell 310 will vary depending on the application, standard dimensions are about a 1 cm². For example, a standard set of dimensions can be about 12.58 mm×12.58 mm overall, about 0.160 mm thick, and a total active area of about 108 mm². For example, in a solar cell 310 that is approximately 12.58 mm×12.58 mm, the upper conductive contact area 312 can be about 0.98 mm wide and the active area can be about 10 mm×10 mm.

The upper conductive contact area 312 of the solar cell 310 may be formed of a variety of conductive materials, e.g., copper, silver, and/or gold-coated silver. In this implementation, it is the n-conductivity cathode (i.e. emitter) side of the solar cell 310 that receives light, and accordingly, the upper conductive contact area 312 is disposed on the cathode side of the solar cell 310. In one embodiment, the upper conductive contact area 312 of the solar cell 310 is wire bonded to the second conductive region 376 of the metallized upper surface 371 of the ceramic substrate 370 via one or more bonding wires 365. The number of bonding wires 365 utilized in a particular implementation can be related, among other things, to the amount of current generated by the solar cell 310. Generally, the greater the current, the greater number of bonding wires 365 that are used.

The bypass diode 360 couples the first conductive region 375 of the metallized upper surface 371 of the ceramic substrate 370 to the second conductive region 376. In one embodiment, a cathode terminal of the bypass diode 360 is connected to the anode terminal of the solar cell 310 via the first conductive region 375 of the ceramic substrate 370 and an anode terminal of the bypass diode 360 is electrically connected to the cathode terminal of the solar cell 310 via the second conductive region 376 of the ceramic substrate 370. The anode terminal of the solar cell 310 is formed by the lower conductive surface 313 of the solar cell 310 as described above and is out-of-view in FIG. 4, but visible in the cross-section of FIG. 5. The cathode terminal of the solar cell 310 is formed by the upper conductive contact area 312 of the solar cell 310 also as described above. The external connection terminals 361, 362 disposed on the metallized upper surface 371 of the ceramic substrate 370 provide for electrical coupling of a device to the solar cell 310 and the bypass diode 360. In some implementations, the connector terminals 361 and 362 correspond to anode and cathode terminals, and are designed to accept receptacle plugs (not shown) for connection to adjacent solar cell receivers.

The upper surface 371 of the ceramic substrate 370 can be metallized by attaching metallization layers 375 and 376 to the substrate. In one embodiment, holes 377 are formed in the metallization layers 375, 376. FIG. 4 shows the ceramic substrate 370 having two metallization layers 375 and 376 attached to the upper substrate surface 371 (the lower metallized surface is out of view in FIG. 4, but visible in the cross-section of FIG. 5). Corresponding bumps 378 (out-of-view in FIG. 4, but visible in the cross-section of FIG. 5) can be formed on the ceramic substrate 310. The bumps 378 are at least partly seated in the holes 377 formed in the metallization layers 375 and 376. The holes 377 in the metallization layers 375 and 376 are then filled with a solder or other type of bonding material such as an adhesive, attaching the metallization layers 375 and 376 to the upper surface 371 of the ceramic substrate 370. The lower surface 372 of the ceramic substrate 370 can be similarly metallized. Alternatively, no bumps 378 are provided on the ceramic substrate 370 and the substrate is relatively planar within normal manufacturing tolerances.

FIG. 5 illustrates a cross-sectional view of the solar cell 310, ceramic substrate 370 and heat sink 350 of the solar cell receiver 300 along the line labeled X-X′ in FIG. 3. The SOE 400, light concentrator 450 and terminals 361, 362 are not illustrated in FIG. 5 for ease of illustration. The upper and lower surfaces 371 and 372 of the ceramic substrate 370 may have bumps 378 that are at least partly seated in holes 377 formed in metallization layers 375, 376 and 379 for attaching the metallization layers to the ceramic substrate 370 as described above. Alternatively, the ceramic substrate 370 is relatively flat within normal manufacturing tolerances. In either case, the upper and lower surfaces 371 and 372 of the ceramic substrate 370 are metallized. The upper metallized surface 371 of the substrate 370 has separated conductive regions 375 and 376 for providing electrically isolated anode and cathode connections to the solar cell 310 as described above.

The solar cell 310 has a conductive lower surface 313 connected to the conductive region 375 of the metallized upper surface 371 of the ceramic substrate 370. In one embodiment, the conductive lower surface 313 of the solar cell 310 forms the anode terminal of the solar cell 310 and the conductive contact area 312 disposed at the upper surface 311 of the solar cell 310 forms the cathode terminal of the solar cell 310. The conductive lower surface 313 of the solar cell 310 is positioned on the first conductive region 375 of the metallized upper surface 371 of the ceramic substrate 370 and electrically isolated from the second conductive region 376 to ensure proper operation of the solar cell 310.

The lower surface 372 of the ceramic substrate 370 also has a metallization layer 379 that is bonded to the heat sink 350 with a highly thermally conductive attach media 380, such as a metal-filled epoxy adhesive or solder. Filling an epoxy adhesive such as silicone with metal increases the thermal conductivity of the interface between the ceramic substrate 370 and the heat sink 350, further improving the heat transfer characteristics of the solar cell receiver 300. In one embodiment, the highly thermally conductive attach media 380 is a metal-filled epoxy adhesive having a thickness t_(epoxy) of approximately 1 to 3 mils. The metal-filled epoxy adhesive can be applied to the lower metallized surface 372 of the ceramic substrate 370, the heat sink 350 or both and then cured to bond the heat sink 350 to the substrate 370. In one embodiment, the heat sink 350 is a single-piece extruded aluminum heat sink as shown in FIG. 3.

The solar cell receiver 300 can be manufactured by providing the metallized ceramic substrate 370 and connecting the conductive lower surface 313 of the solar cell 310 to the first conductive region 375 of the metallized upper surface 371 of the substrate 370. The conductive contact area 312 disposed at the upper surface 311 of the solar cell 310 is connected to the second conductive region 376 of the metallized upper surface 371 of the ceramic substrate 370, e.g. via one or more bond wires 365. The heat sink 350 is bonded to the lower metallized surface 372 of the ceramic substrate 370 with the metal-filled epoxy adhesive 380.

In various implementations described herein, a triple-junction III-V compound semiconductor solar cell is employed, but other types of solar cells could be used depending upon the application. The solar cells 310 may be made from, e.g., silicon (including amorphous, nanocrystalline, or protocrystalline), cadmium telluride, CIGS (copper indium gallium diselenide), CIS (chalcopyrite films of copper indium selenide (CuInSe₂)), gallium arsenide (e.g., GaAs multijunctions), light absorbing dyes (e.g., ruthenium metalorganic dye), or organic semiconductors (e.g., polyphenylene vinylene, copper phthalocyanine or carbon fullerenes).

Since a single solar cell module 200 may not produce sufficient electricity for a given application, two or more solar cell modules 200 may be grouped together into an array. These arrays are sometimes referred to as “panels” or “solar panels.”

While particular embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that, based upon the teachings herein, changes and modifications may be made without departing from this invention and its broader aspects and, therefore, the appended claims are to encompass within their scope all such changes and modifications as are within the scope of this invention. Furthermore, it is to be understood that the invention is solely defined by the appended claims.

It will be understood by those within the art that, in general, terms used herein, and especially in the appended claims (e.g., bodies of the appended claims) are generally intended as “open” terms (e.g., the term “including” should be interpreted as “including but not limited to,” the term “having” should be interpreted as “having at least,” the term “includes” should be interpreted as “includes but is not limited to,” “comprise” and variations thereof, such as, “comprises” and “comprising” are to be construed in an open, inclusive sense, that is as “including, but not limited to,” etc.). It will be further understood by those within the art that if a specific number of an introduced claim recitation is intended, such an intent will be explicitly recited in the claim, and in the absence of such recitation no such intent is present. For example, as an aid to understanding, the following appended claims may contain usage of the introductory phrases “at least one” and “one or more” to introduce claim recitations. However, the use of such phrases should not be construed to imply that the introduction of a claim recitation by the indefinite articles “a” or “an” limits any particular claim containing such introduced claim recitation to inventions containing only one such recitation, even when the same claim includes the introductory phrases “one or more” or “at least one” and indefinite articles such as “a” or “an” (e.g., “a” and/or “an” should typically be interpreted to mean “at least one” or “one or more”); the same holds true for the use of definite articles used to introduce claim recitations. In addition, even if a specific number of an introduced claim recitation is explicitly recited, those skilled in the art will recognize that such recitation should typically be interpreted to mean at least the recited number (e.g., the bare recitation of “two recitations,” without other modifiers, typically means at least two recitations, or two or more recitations). 

1. A solar cell module to convert light to electricity comprising: a housing comprising a first side and an opposing spaced-apart second side; a plurality of lenses on the first side of the housing; a plurality of solar cell receivers on the second side of the housing, each of the plurality of solar cell receivers comprising: a III-V compound semiconductor multifunction solar cell including a first surface and a second surface; a bypass diode coupled with the solar cell; a heat sink positioned below the second surface of the solar cell and thermally coupled to the solar cell; at least one optical element positioned above the first surface to guide the light onto the solar cell; each of said solar cell receivers being disposed in an optical path of one of the plurality of lenses, wherein the lens and the at least one optical element concentrate the light onto the respective solar cell by a factor of 1000 or more to generate in excess of 25 watts of peak power.
 2. The solar cell module of claim 1, wherein the at least one optical element includes a hollow secondary optical element disposed within the optical path and including an entry aperture that faces away from the solar cell to receive the light, an exit aperture that faces towards the solar cell to direct the light towards the solar cell, the secondary optical element including a tapered shape with the entry aperture being larger than the exit aperture.
 3. The solar cell module of claim 1, wherein the at least one optical element includes a solid glass concentrator disposed within the optical path and including an optical inlet that faces away from the solar cell and an optical outlet that faces towards the solar cell, the concentrator including a tapered shape with the optical inlet being larger than the optical outlet.
 4. The solar cell module of claim 1, wherein the plurality of lenses on the first side of the housing are arranged in a 3×5 array.
 5. The solar cell module of claim 1, wherein the housing and the plurality of lenses form an enclosed interior with the solar cell positioned within the enclosed interior.
 6. The solar cell module of claim 1, wherein the plurality of lenses are constructed as a unified lens sheet that extends across the first side of the housing.
 7. The solar cell module of claim 1, further comprising a plurality of covered openings in the housing to facilitate air flow through the housing.
 8. A solar cell module to convert light to electricity comprising: a housing; a plurality of lenses positioned at a first side of the housing; a plurality of solar cell receivers positioned at an opposing second side of the housing and each comprising: an optical element; a ceramic substrate having a first metallized surface and an opposing second metallized surface, the first metallized surface having separated conductive regions; a III-V compound semiconductor multijunction solar cell having an anode terminal electrically connected to a first one of the conductive regions of the ceramic substrate and a cathode terminal electrically connected to a second one of the conductive regions; a bypass diode connected across the first and second conductive regions of the ceramic substrate in parallel with the solar cell ; and a heat sink bonded to the second metallized surface of the ceramic substrate with a thermally conductive attach media; each of said solar cell receivers being disposed in an optical path of one of the plurality of lenses, wherein the lenses and the optical element concentrate the light onto the respective solar cell by a factor of 1000 or more to generate in excess of 25 watts of peak power.
 9. The solar cell module of claim 8, further comprising a hollow secondary optical element disposed within the optical path and including an entry aperture that faces away from the solar cell to receive the light, an exit aperture that faces towards the solar cell to direct the light towards the solar cell, the second optical element including a tapered shape with the entry aperture being larger than the exit aperture.
 10. The solar cell module of claim 9, wherein the optical element includes a solid glass concentrator disposed within the optical path between the solar cell and the secondary optical element, the concentrator including an optical inlet that faces towards the secondary optical element and an optical outlet that faces towards the solar cell, the concentrator including a tapered shape with the optical inlet being larger than the optical outlet.
 11. The solar cell module of claim 8, wherein the plurality of lenses on the first side of the housing are arranged in a 3×5 array.
 12. The solar cell module of claim 8, wherein the housing and the plurality of lenses form an enclosed interior with the solar cell and the diode positioned within the enclosed interior.
 13. The solar cell module of claim 8, wherein the plurality of lenses are constructed as a unified lens sheet that extends across the first side of the housing.
 14. The solar cell module of claim 8, further comprising a plurality of openings in the housing to facilitate air flow through the housing, each of the openings including a cover that extends across the opening.
 15. A solar cell module to convert light to electricity comprising: a housing with a plurality of lenses that form an enclosed interior space; a plurality of solar cell receivers connected to the housing and spaced away from the plurality of lenses, each of the plurality of solar cell receivers comprising: a ceramic substrate having a first metallized surface and an opposing second metallized surface, the first metallized surface having separated conductive regions; a III-V compound semiconductor multijunction solar cell having an anode terminal electrically connected to a first one of the conductive regions of the ceramic substrate and a cathode terminal electrically connected to a second one of the conductive regions; a bypass diode connected across the first and second conductive regions of the ceramic substrate in parallel with the solar cell; a secondary optical element positioned above the solar cell and including a tapered shape with a larger inlet that faces away from the solar cell and a smaller outlet that faces towards the solar cell; a concentrator positioned above the solar cell; each of said solar cell receivers, secondary optical elements, and concentrators being disposed in an optical path of one of the plurality of lenses, wherein the lens, the secondary optical element, and the concentrator concentrate the light onto the respective solar cell by a factor of 1000 or more to generate in excess of 25 watts of peak power.
 16. The solar cell module of claim 15, further comprising thermally coupled to the solar cell and positioned on an opposite side of the solar cell from the concentrator and the secondary optical element.
 17. The solar cell module of claim 15, wherein the housing forms a rectangular shape and the plurality of lenses are arranged in a 3×5 array.
 18. The solar cell module of claim 15, wherein the plurality of lenses are constructed as a unified lens sheet that extends across a first side of the housing. 